# Service difficulty reports: N205AU, cancelled May 30, 2018

A list on [N205AU, cancelled May 30, 2018](https://openairdocs.org/deregistered/N205AU-2018-05-30.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 61 reports

- [SDR F3LA99119](https://openairdocs.org/sdr/F3LA99119.md): Axle · corroded · Sep 4, 1999 · N205AU · Boeing 737201 · Nose/Tail Landing Gear Strut/Axle
  > DEN - DURING C-4 CHECK, INSPECTION REPORTED DAMAGE FROM CORROSION PITTING ON NOSE LANDING GEAR RT AXLE. REPLACED INNER CYLINDER ASSY PER BOEING MM 32-21-11. (M)
- [SDR F3LA99115](https://openairdocs.org/sdr/F3LA99115.md): Wire · failed · Aug 22, 1999 · N205AU · Boeing 737201 · Light System Wiring
  > DEN - DURING C-4 CHECK INSPECTION, REPORTED EMERGENCY EXIT SIGN INOPERATIVE AT ROW 9 LEFT SIDE. MAINTENANCE REPAIRED WIRING AT SEAT 9C FOR EMERGENCY EXIT SIGN. (M)
- [SDR F3LA99043](https://openairdocs.org/sdr/F3LA99043.md): Drag Brace · cracked · Jun 4, 1999 · N205AU · Boeing 737201 · Nose/Tail Landing Gear
  > DEN - DURING SERVICE CHECK, INSPECTION REPORTED NOSE LANDING GEAR UPPER DRAG BRACE BEARING MIGRATING AT ACTUATOR ATTACH POINT. UPON FURTHER INSPECTION, FOUND 1 INCH CRACK IN NOSE GEAR UPPER DRAG BRACE A-FRAME ON RT SIDE OF WEB. MAINTENANCE INSTALLED NEW DRA
- [SDR F3LA99004](https://openairdocs.org/sdr/F3LA99004.md): Wire · broken · Feb 17, 1999 · N205AU · Boeing 737201 · Light System Wiring
  > DEN - DURING A-6 CHECK, INSPECTION REPORTED FLOOR PROXIMITY LIGHTING AT ROWS 16, 17 AND 18 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRING AND SYSTEM CHECKED OK. (M)
- [SDR F3LA99001](https://openairdocs.org/sdr/F3LA99001.md): Skin · damaged · Jan 5, 1999 · N205AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > DEN - FLT 850 - UPON ARRIVAL, MAINTENANCE REPORTED HOLE IN FUSELAGE, AFT OF FORWARD LAV SERVICE DOOR STATION 328, STRINGER 24R TO STRINGER 25R. MAINTENANCE FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-5. (M)
- [SDR F3LA98163](https://openairdocs.org/sdr/F3LA98163.md): Skin · cracked · Aug 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED A 3 INCH CRACK IN NOSE WHEEL WELL SKIN, BS 245.6 TO 248.6, WL 168.5. A.125 INCH CRACK AT RIVET, BS 244.1, W 165.5, AND A.125 INCH CRACK AT BS 243.1, WL 164.3. MAINTENANCE REPAIRED DAMAGED AREAS PER SRM 51-40
- [SDR F3LA98080](https://openairdocs.org/sdr/F3LA98080.md): Gcu · failed · Jun 14, 1998 · N205AU · Boeing 737201 · AC Regulator
  > PHX - FLT 429 - DURING DESCENT INTO PHX, FLIGHT CREW REPORTED NR 1 GENERATOR OFF BUS LIGHT ILLUMINATED FOLLOWED BY THE SMELL OF ELECTRICAL SMOKE WITH A SMALL AMOUNT OF VISIBLE SMOKE NOTICED. COMPLIED WITH SMOKE REMOVAL CHECKLIST AND SMOKE DISSIPATED. AIRCRAF
- [SDR F3LA98089](https://openairdocs.org/sdr/F3LA98089.md): Angle · corroded · Jun 5, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON MAIN EQUIPMENT BAY RIGHT INTERCOSTAL LOWER OUTBOARD SUPPORT ANGLE AT BS 353, RBL 12, WL 146. MAINTENANCE REPAIRED PER EO 98-0502. (M)
- [SDR F3LA98088](https://openairdocs.org/sdr/F3LA98088.md): Frame · cracked · May 29, 1998 · N205AU · Boeing 737201 · Cargo/Baggage Doors
  > PAE - DURING C-CHECK INSPECTION REPORTED CRACK IN FORWARD CARGO DOOR LOWER FORWARD FRAME IN OUTBOARD RADIUS OF LATCH ARM. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SB 737-52-1100 AND MM 52-31-0. CYCLES: 2,451. (X)
- [SDR F3LA98087](https://openairdocs.org/sdr/F3LA98087.md): Skin · cracked · May 29, 1998 · N205AU · Boeing 737201 · Wing, Plate/Skin
  > PAE - DURING C-CHECK INSPECTION, REPORTED CRACK ABOVE NR 2 LEADNG EDGE PYLON. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM'S 51-10-1, 51-30-2, AND 57-30-4. CYCLES: 2,451.0. (X)
- [SDR F3LA98086](https://openairdocs.org/sdr/F3LA98086.md): Splice · cracked · May 29, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN BS 727 BULKHEAD TO FLOORBEAM SUPPORT SPLICE AFT FLANGE, LBL 25, WL 202. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-1, 51-10-2, 51-20-1 AND 51-30-2. (M)
- [SDR F3LA98084](https://openairdocs.org/sdr/F3LA98084.md): Doubler · corroded · May 29, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON INNER MOUNTING DOUBLER FOR FORWARD LAVATORY DRAIN TUBE, BS 270, STRINGER 23R. MAINTENANCE REMOVED DAMAGED DOUBLER, FABRICATED REPLACMENT PART AND REPAIRED PER SRM 51-20-4, 51-30-2 AND 53-10-1. (M)
- [SDR F3LA98083](https://openairdocs.org/sdr/F3LA98083.md): Intercostal · cracked · May 29, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - DURING C-CHECK INSPECTION, REPORTED CRACK ON INTERCOSTAL, AFT SIDE AT BS 294.5 STRINGER 7L. MAINTENANCE REMOVED INTERCOSTAL, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-3 FIG 2. (M)
- [SDR F3LA98081](https://openairdocs.org/sdr/F3LA98081.md): Skin · cracked · May 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN FORWARD ENTRY DOOR OUTER SKIN, LOWER HINGE CUTOUT, UPPER AFT CORNER. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SB 737-52-1096 AND SRM 51-30-2. (M)
- [SDR F3LA98079](https://openairdocs.org/sdr/F3LA98079.md): Stringer · cracked · May 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - DURING C-CHECK, INSPECTION REPORTED CRACK 1 INCH ABOVE STRINGER 12L, BS 294.5. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2, 51-40-3, FIG 1 AND 53-10-4. (M)
- [SDR F3LA98078](https://openairdocs.org/sdr/F3LA98078.md): Stringer · cracked · May 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN CROWN OF STRINGER 7L, BS 295. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-3, FIG 1. (M)
- [SDR F3LA98077](https://openairdocs.org/sdr/F3LA98077.md): Skin · cracked · May 29, 1998 · N205AU · Boeing 737201 · Wing, Plate/Skin
  > PAE - DURING C-CHECK, INSPECTION REPORTED 1 INCH CRACK IN SKIN ABOVE NR 1 ENGINE PYLON, LEFT WING LEADING EDGE. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 57-30-04. (M)
- [SDR F3LA98076](https://openairdocs.org/sdr/F3LA98076.md): Frame · corroded · May 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, Frame
  > PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON FRAME AND SHEAR TIE AT BS 360, RBL 8-13, BETWEEN STRINGER 27R AND 28R. MAINTENANCE REMOVED DAMAGED AREA (6 INCH BY 4 INCH BY.006 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-1
- [SDR F3LA98070](https://openairdocs.org/sdr/F3LA98070.md): Shear Tie · cracked · May 29, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - DURING C-CHECK INSPECTION, REPORTED 1.8 INCH CRACK IN SHEAR TIE AT BS 294 BETWEEN STRINGER 12L AND 14L. MAINTENANCE FABRICATED NEW SHEAR TIE AND REPAIRED PER SRM 51-10-2 AND 51-30-2. (M)
- [SDR F3LA98062](https://openairdocs.org/sdr/F3LA98062.md): Skin · cracked · May 29, 1998 · N205AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN AFT SERVICE DOOR SKIN ABOVE LOWER HINGE CUTOUT AT BS 949, STRINGER 14R, WL 220. MAINTENANCE REMOVED DAMAGED AREA, 1.5 INCH BY 2.5 INCH. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 52-00-3. (M)
- [SDR F3LA980529](https://openairdocs.org/sdr/F3LA980529.md): Frame · cracked · May 29, 1998 · N205AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN FORWARD CARGO DOOR UPPER AFT FRAME. MAINTENANCE REMOVED DAMAGED FRAME. FABRICATED REPLACEMENT PART AND REPAIRED PER SRM 51-30-2. (M)
- [SDR F3LA98052](https://openairdocs.org/sdr/F3LA98052.md): Skin · corroded · May 26, 1998 · N205AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON INTERNAL SKIN AT BS 353-356, RBL 3. MAINTENANCE REPAIRED SKIN PER SRM 53-30-3, FIG 28. (M)
- [SDR F3LA98012](https://openairdocs.org/sdr/F3LA98012.md): Skin · cracked · Apr 1, 1998 · N205AU · Boeing 737201 · Wing, Plate/Skin
  > DEN - PRIOR TO DEPARTURE, MAINTENANCE REPORTED ONE.25 INCH CRACK IN LEFT WING LEADING EGE SKIN AT WBL 165.0. MAINTENANCE REPAIRED DAMAGED AREA PER SRM 57-30-4, PAGE 4. (M)
- [SDR F3LA98009](https://openairdocs.org/sdr/F3LA98009.md): Wire · loose · Mar 17, 1998 · N205AU · Boeing 737201 · Light System Wiring
  > PHX - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 4 A, B, C INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SECURED WIRING HARNESS AND SYSTEM CHECKED OK. (M)
- [SDR F3LA98006](https://openairdocs.org/sdr/F3LA98006.md): Line · failed · Mar 8, 1998 · N205AU · Boeing 737201 · Hydraulic System, Main
  > SFO - ON INBOUND FLIGHT TO SFO, FLIGHT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULIC PRESSURE AND FLUID. USED ALTERNATE FLAP SYSTEM AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE 'A' SYSTEM HYDRAULIC PRESSURE LINE IN AFT FLAP WELL, BOTH 'A' SYSTEM H
- [SDR F3LA97157](https://openairdocs.org/sdr/F3LA97157.md): Light · inoperative · Nov 16, 1997 · N205AU · Boeing 737201 · Emergency Lighting
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED AFT RT EMERGENCY EXIT LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. REPLACED LIGHT ASSEMBLY AND CHECKED OK. (M)
- [SDR F3LA97150](https://openairdocs.org/sdr/F3LA97150.md): Control Panel · failed · Sep 27, 1997 · N205AU · Boeing 737201 · Autopilot System
  > OMA - UPON ARRIVAL, FLIGHT CREW REPORTED ELECTRICAL ODOR IN COCKPIT. REPLACED AUTOPILOT CONTROL PANEL AND CHECKED OK. (M)
- [SDR F3LA97149](https://openairdocs.org/sdr/F3LA97149.md): Line · failed · Sep 24, 1997 · N205AU · Boeing 737201 · Hydraulic System, Main
  > AIR TURN BACK. UPON ROTATION, FLIGHT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULI CS AND DECLARED AN EMERGENCY. AIRCRAFT LEFT RUNWAY UPON LANDING AND GOT STUCK IN THE MUD. PASSENGERS WERE EVACUATED. REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE IN PYLON AND BO
- [SDR F3LA97131](https://openairdocs.org/sdr/F3LA97131.md): Wire · broken · Jun 21, 1997 · N205AU · Boeing 737201 · Light System Wiring
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 4L INOPERATIVE. MAINTENANCE SPLICED BROKEN WIRE UNDER SEAT WITH BUTT CONNECTOR AND SECURED WIRE ROUTING UNDER SEAT FRAME. SYSTEM CHECKED OKAY. AIRFRAME TOTAL TIME: 72,075.1 HR
- [SDR F3LA97133](https://openairdocs.org/sdr/F3LA97133.md): Wire · failed · Jun 6, 1997 · N205AU · Boeing 737201 · Light System Wiring
  > DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 7A INOPERATIVE. MAINTENANCE INSTALLED NEW BUTT SPLICE SYSTEM CHECKED OKAY. (X)
- [SDR F3LA97129](https://openairdocs.org/sdr/F3LA97129.md): Battery Pack · discharged · Jun 6, 1997 · N205AU · Boeing 737201 · Emergency Lighting
  > DEN - FLT 18 - UPON ARRIVAL, FLIGHT CREW REPORTED FORWARD SECTION OF FLOOR PROXIMITY LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND SYSTEM CHECKED OK. (M)
- [SDR F3LA97098](https://openairdocs.org/sdr/F3LA97098.md): Bulb · failed · Mar 16, 1997 · N205AU · Boeing 737201 · Emergency Lighting
  > DEN - UPON ARRIVAL, FLIGHT CREW REPORTED L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED LAMP AND CHECKED OK. (M)
- [SDR F3LA97097](https://openairdocs.org/sdr/F3LA97097.md): Skin · dented · Mar 7, 1997 · N205AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > FUSELAGE DENTS BETWEEN BS 360 AND 409. REMOVED SKIN FROM BS 360 TO 440, STRINGER 19R TO 24R. FABRICATED AND INSTALLED REPLACEMENT SKIN AND REPAIR IAW EWO 97-0080. REF WORK ORDER 214932 FUSELAGE 153/7-133 AND SRM. (M)
- [SDR F3LA97096](https://openairdocs.org/sdr/F3LA97096.md): Skin · cracked · Mar 7, 1997 · N205AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - A.5 INCH CRACK IN THE UPPER FORWARD CORNER OF THE FORWARD ENTRY DOOR CUTOUT SKIN. WHILE ACCOMPLISHING EA 53-737-023 INADVERTENTLY OVERSIZED 34 HOLES ABOVE ALLOWABLE LIMITS IN BOEING SB 737-53-1163. REPAIRED DAMAGED HOLES IAW TRAMCO EWO 97-0140 BY OVER
- [SDR F3LA97093](https://openairdocs.org/sdr/F3LA97093.md): Skate Angle · cracked · Feb 26, 1997 · N205AU · Boeing 737201 · Vertical Stabilizer
  > RIGHT VERTICAL STAB AFT MOUNT LUG INBOARD SKATE ANGLE CRACKED. REMOVED RIGHT VERTICAL STAB AFT MOUNTING LUG INBOARD SKATE ANGLE. FABRICATED REPAIR ANGLE FROM MATERIAL OF 7075-0.071 AND HEAT TREATED BY GIDDENS INDUSTRIES, INC TO 7075-T6, PO NR 1ML212756. IN
- [SDR F3LA97052](https://openairdocs.org/sdr/F3LA97052.md): Bracket · corroded · Feb 10, 1997 · N205AU · Boeing 737201 · Fuselage Miscellaneous Structure
  > PAE - FOUND CORROSION (C53-107-01) ON AFT AIRSTAIR HINGE SUPPORT BRACKET AT BS 982, LBL 40, WL 208. REMOVED CORROSION FROM AFT AIRSTAIR HINGE SUPPORT BRACKET IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. FABRICATED FLOOR SUPPORT PLATE AND FILL
- [SDR F3LA97051](https://openairdocs.org/sdr/F3LA97051.md): Skin · cracked · Feb 10, 1997 · N205AU · Boeing 737201 · Service Doors
  > PAE - FORWARD SERVICE DOOR LOWER HINGE CUTOUT UPPER CORNER IS CRACKED.125 INCH IN LENGTH. REPAIRED CRACK BY STOP DRILLING AND INSTALLING EXTERNAL DOUBLER IAW TRAMCO EWO 97-0094. (M)
- [SDR F3LA97048](https://openairdocs.org/sdr/F3LA97048.md): Floor Beam · corroded · Feb 10, 1997 · N205AU · Boeing 737201 · Fuselage Main, Floor Beam
  > PAE - FLOOR BEAM UPPER CHORD AT BS 277 HAS TWO.625 INCH DIAMETER HOLES AT LBL 17 AND LBL 24, WL 208. CORROSION WAS DISCOVERED AT BS 277 LBL 17, LBL 20, AND LBL 25 WL 208. REMOVED CORROSION ON FLOOR BEAM FOUND TO BE OUT OF LIMITS, IAW 53-10-1, REPAIRED FLOOR
- [SDR F3LA97049](https://openairdocs.org/sdr/F3LA97049.md): Seat Track · corroded · Feb 9, 1997 · N205AU · Boeing 737201 · Fuselage, Seat/Cargo Attach Fittings
  > PAE - WHILE WORKING INTERIOR 00171, FOUND CORROSION ON SEAT TRACK AT RBL 25, BS 344-BS 360. REMOVED CORROSION ON SEAT TRACK AT RBL 25, BS 344-BS 360, WL 208, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED SEAT TRACK FROM BS 344-BS 360, FABRICATED SEAT TR
- [SDR F3LA97053](https://openairdocs.org/sdr/F3LA97053.md): Stringer · cracked · Feb 8, 1997 · N205AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
  > PAE - AT STATION 500B PLUS 2.5, STRINGER 16L IS CRACKED, LENGTH OF CRACK.25 INCH. CUTOUT DAMAGED AREA AND REPAIRED PER TRAMCO EWO NR 97-0115 AND BOEING SB 737-53-1145. WORK ACCOMPLISHED ON TRAMCO WORK ORDER NR INTERIOR 262. (M)
- [SDR F3LA97046](https://openairdocs.org/sdr/F3LA97046.md): Floor Beam · corroded · Feb 6, 1997 · N205AU · Boeing 737201 · Fuselage Main, Floor Beam
  > PAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD, BS 360, RBL 1 TO LBL 11, WL 208.1. FOUND CORROSION BEYOND LIMITS. REMOVED BS 360, WL 208.1 CHORD FROM LBL 13 TO RBL 15. FABRICATED AND INSTALLED REPAIR. ALL WORK DONE IAW SRM 53-10-1, 53-10-9, 5
- [SDR F3LA97037](https://openairdocs.org/sdr/F3LA97037.md): Floor Beam · corroded · Feb 6, 1997 · N205AU · Boeing 737201 · Fuselage Main, Floor Beam
  > PAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 344, RBL 9 TO LBL 65. FOUND CORROSION BEYOND LIMITS PER SRM 52-10-1. REMOVED CHORD FROM LBL 65 TO RBL 65. FABRICATED AND INSTALLED NEW CHORD. ALL WORK PERFORMED IAW SRM 51-10-6, 53-10-2, 53-10
- [SDR F3LA97036](https://openairdocs.org/sdr/F3LA97036.md): Floor Beam · corroded · Feb 5, 1997 · N205AU · Boeing 737201 · Fuselage Main, Floor Beam
  > PAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 328, RBL 60 - LBL 30, WL 208.1. REMOVED CORROSION ON FLOOR BEAM UPPER CHORD BS 328. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED UPPER CHORD AND REPAIR ANGLES FROM 7075-T6.090 T-ANGLE
- [SDR F3LA97035](https://openairdocs.org/sdr/F3LA97035.md): Skin · gouged · Feb 4, 1997 · N205AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - AFT CARGO DOOR EXTERNAL SKIN GOUGED 28 INCH FROM FWD EDGE. BLENDED GOUGED AREA IN EXTERNAL SKIN OF AFT CARGO DOOR 28 INCH IN FROM FORWARD EDGE AND 21 INCH DOWN FROM EDGE. DAMAGED AREA FOUND TO BE OUT LIMITS IAW SRM 52-00-2. REMOVED, FABRICATED DOUBLER
- [SDR F3LA97034](https://openairdocs.org/sdr/F3LA97034.md): Seat Track · corroded · Feb 4, 1997 · N205AU · Boeing 737201 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND CORROSION (C53-107-01), ON SEAT TRACK BS 344-360, LBL 45, WL 208. BLENDED OUT CORROSION AT BS 344-360, LBL 45, WL 208. BLENDED OUT CORROSION AT BS 344-360, LBL 45, WL 208 IN AN AREA 6 INCH BY 1 INCH BY.020 INCH. ORIGINAL THICKNESS. 270 INCH OF SEAT
- [SDR F3LA97033](https://openairdocs.org/sdr/F3LA97033.md): Floor Beam · corroded · Feb 4, 1997 · N205AU · Boeing 737201 · Fuselage Main, Floor Beam
  > PAE - FOUND CORROSION (C53-107-02) ON FLOOR BEAM UPPER CHORD BS 294, LBL 21 TO RBL 60, WL 208.1. REMOVED CORROSION ON FLOOR BEAM UPPER CHORD BS 294, LBL 21 TO RBL 60, WL 208.1 IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED UPPER CHORD F
- [SDR F3LA97032](https://openairdocs.org/sdr/F3LA97032.md): Access Door · cracked · Feb 4, 1997 · N205AU · Boeing 737201 · Auxiliary Power Unit (APU) Doors
  > APU ACCESS DOOR MOST AFT RIB RIGHT CORNER CRACKED. STOP DRILLED CRACK END USING.125 INCH DRILL, CRACK WAS FOUND TO BE 2 INCHES IN LENGTH. REMOVED DAMAGED AREA AND INSTALLED FABRICATED REPAIR PARTS FROM STOCK MATERIAL OF 2024-T3.050 IAW SRM 51-10-1, 52-40-1
- [SDR F3LA97031](https://openairdocs.org/sdr/F3LA97031.md): Skin · dented · Feb 4, 1997 · N205AU · Boeing 737201 · Cargo/Baggage Doors
  > PAE - FORWARD CARGO DOOR EXTERNAL SKIN DENTED 18-20 INCHES DOWN FROM TOP EDGE AND 15-16 INCHES IN FROM AFT EDGE. DENT IN FORWARD CARGO DOOR EXTERNAL SKIN 18-20 INCHES DOWN FROM TOP EDGE AND 15-16 INCHES IN FROM AFT EDGE. FOUND TO BE OUT OF LIMITS IAW SRM 52-
- [SDR F3LA97030](https://openairdocs.org/sdr/F3LA97030.md): Skin · dented · Jan 31, 1997 · N205AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - DENT ON SKIN AT BS 388.5, 4 INCH ABOVE STRINGER 19L. REMOVED DAMAGED SKIN ON BS 388.5, 4 INCHES ABOVE STRINGER 19L. FABRICATED THE DOUBLER FROM 2024-T3.050 MATERIAL. SEALED AND INSTALLED WITH RIVETS PER SRM 53-30-3. (M)
- [SDR F3LA97029](https://openairdocs.org/sdr/F3LA97029.md): Skin · dented · Jan 30, 1997 · N205AU · Boeing 737201 · Fuselage Main, Plate/Skin
  > PAE - DENT IN SKIN AT BS 875-879, BETWEEN STRINGER 17R-18R. FOUND DENT TO BE OUT OF LIMITS IAW SRM 53-30-01. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER FROM 2024-T3.063 SHEET STOCK. DOUBLER INSTALLED WET SEALANT. ALL WORK DONE IAW SRM 53-30-3 FIG

Next page: https://openairdocs.org/deregistered/N205AU-2018-05-30/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N205AU' AND deregistration_id = 'N205AU-2018-05-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N205AU-2018-05-30/reports

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